#include "aoview.h"
#include <math.h>
-static int pad_pres;
-static int pad_accel;
-static int pad_pres_total;
-static int pad_accel_total;
static double pad_lat_total;
static double pad_lon_total;
static int pad_alt_total;
-static int npad;
static int npad_gps;
static int prev_tick;
static double prev_accel;
double max_accel;
if (!strcmp(state->state, "pad")) {
- if (npad < NUM_PAD_SAMPLES) {
- pad_accel_total += state->flight_accel;
- pad_pres_total += state->flight_pres;
- if (state->locked) {
- pad_lat_total += state->lat;
- pad_lon_total += state->lon;
- pad_alt_total += state->alt;
- npad_gps++;
- }
- npad++;
+ if (state->locked && npad_gps < NUM_PAD_SAMPLES) {
+ pad_lat_total += state->lat;
+ pad_lon_total += state->lon;
+ pad_alt_total += state->alt;
+ npad_gps++;
}
- if (npad <= NUM_PAD_SAMPLES) {
- pad_pres = pad_pres_total / npad;
- pad_accel = pad_accel_total / npad;
- if (npad_gps) {
- pad_lat = pad_lat_total / npad_gps;
- pad_lon = pad_lon_total / npad_gps;
- pad_alt = pad_alt_total / npad_gps;
- }
- }
- if (npad == NUM_PAD_SAMPLES) {
- npad++;
- min_pres = pad_pres;
- min_accel = pad_accel;
+ if (state->locked && npad_gps <= NUM_PAD_SAMPLES) {
+ pad_lat = pad_lat_total / npad_gps;
+ pad_lon = pad_lon_total / npad_gps;
+ pad_alt = pad_alt_total / npad_gps;
}
+ min_pres = state->ground_pres;
+ min_accel = state->ground_accel;
}
if (state->flight_pres < min_pres)
min_pres = state->flight_pres;
if (state->flight_accel < min_accel)
min_accel = state->flight_accel;
- altitude = aoview_pres_to_altitude(state->flight_pres) - aoview_pres_to_altitude(pad_pres);
- accel = (pad_accel - state->flight_accel) / 27.0;
+ altitude = aoview_pres_to_altitude(state->flight_pres) - aoview_pres_to_altitude(state->ground_pres);
+ accel = (state->ground_accel - state->flight_accel) / 27.0;
velocity = state->flight_vel / 2700.0;
- max_accel = (pad_accel - min_accel) / 27.0;
+ max_accel = (state->ground_accel - min_accel) / 27.0;
ticks = state->tick - prev_tick;
temp = ((state->temp / 32767.0 * 3.3) - 0.5) / 0.01;
battery = (state->batt / 32767.0 * 5.0);
prev_tick = state->tick;
aoview_table_start();
- if (npad >= NUM_PAD_SAMPLES)
+ if (npad_gps >= NUM_PAD_SAMPLES)
aoview_table_add_row("Ground state", "ready");
else
- aoview_table_add_row("Ground state", "preparing (%d)",
- NUM_PAD_SAMPLES - npad);
+ aoview_table_add_row("Ground state", "waiting for gps (%d)",
+ NUM_PAD_SAMPLES - npad_gps);
aoview_table_add_row("Rocket state", "%s", state->state);
aoview_table_add_row("Callsign", "%s", state->callsign);
aoview_table_add_row("Rocket serial", "%d", state->serial);
- aoview_table_add_row("RSSI", "%ddB", state->rssi);
+ aoview_table_add_row("RSSI", "%ddBm", state->rssi);
aoview_table_add_row("Height", "%dm", altitude);
aoview_table_add_row("Max height", "%dm",
aoview_pres_to_altitude(min_pres) -
- aoview_pres_to_altitude(pad_pres));
+ aoview_pres_to_altitude(state->ground_pres));
aoview_table_add_row("Acceleration", "%gm/s²", accel);
aoview_table_add_row("Max acceleration", "%gm/s²", max_accel);
aoview_table_add_row("Velocity", "%gm/s", velocity);
aoview_table_add_row("Battery", "%gV", battery);
aoview_table_add_row("Drogue", "%gV", drogue_sense);
aoview_table_add_row("Main", "%gV", main_sense);
- aoview_table_add_row("Pad altitude", "%dm", aoview_pres_to_altitude(pad_pres));
+ aoview_table_add_row("Pad altitude", "%dm", aoview_pres_to_altitude(state->ground_pres));
aoview_table_add_row("Satellites", "%d", state->nsat);
if (state->locked) {
aoview_state_add_deg("Latitude", state->lat);
void
aoview_state_new(void)
{
- pad_pres = 0;
- pad_accel = 0;
- pad_pres_total = 0;
- pad_accel_total = 0;
pad_lat_total = 0;
pad_lon_total = 0;
pad_alt_total = 0;
- npad = 0;
npad_gps = 0;
prev_tick = 0;
prev_accel = 0;